The stability under longitudinal compression of flat symmetric corrugated-core sandwich plates with simply supported loaded edges and simply supported or clamped unloaded edges /

Bibliographic Details
Main Author: Seide, Paul
Corporate Authors: Knovel (Firm), United States. National Advisory Committee for Aeronautics
Format: Government Document eBook
Language:English
Published: Washington, D.C. : National Advisory Committee for Aeronautics, 1952.
Series:Technical note (United States. National Advisory Committee for Aeronautics) ; no. 2679.
Subjects:
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Call Number: TA660.P6
 
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